Airframe/engine Compatibility Plan. General Electric Engine. Commercial Supersonic Transport Program. Phase Ii-c Report PDF Download
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Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Get Book Here
Book Description
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 828
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Book Description
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
This document describes the performance guarantees for the Boeing Model 733-390 powered by General Electric engines, the Model 733-394 powered by Pratt and Whitney engines, and the 733 prototype airplane.
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Book Description
This specification describes the aircraft engine installation. The essential physical and functional characteristics are noted and the design requirements are specified in some detail. Ground and flight tests which will ensure that the installation is satisfactory are established. The specific engine installation covered is the GE4/J5G. (Author).
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 21
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Book Description
This specification describes the principal physical and functional characteristics of the control systems necessary to start, set, vary thrust, and stop the General Electric GE4/J5G engine. The design requirements are specified. Ground and flight tests to ensure that the control systems are satisfactory have been established. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 117
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Book Description
Throughout Phase II-C, as in earlier phases of the SST Program, The Boeing Company has maintained a program of design analysis and performance evaluation, with the coordinated participation of both engine contractors. As a result, the General Electric GE4/J5P powered B-2707 (GE) and the Pratt and Whitney Aircraft JFT17A-21B powered B-2707 (P and WA) airplanes are very competitive in terms of overall airplane performance criteria, and either would make an outstanding airline airplaned. The purpose of this document is to report the technical evaluation of the two engines. Considerations in this evaluation include engine/airplane matching and performance, engine design, installation compatibility, development plan, development risk, and growth potential.
Author: BOEING CO RENTON WA.
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
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Book Description
This specification describes the engine inlet anti-icing system and establishes its requirements, and testing objectives. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be determined after prototype flight testing.
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
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Book Description
This specification establishes the requirements for performance, design, test and qualification for the Aircraft engine Installation Subsystem. The subsystem is used to provide the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem is also used to provide mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem requires fuel, air flow, electrical and airframe support and control inputs for its operation. These are provided by the airframe fuel, air inlet, air inlet control, electrical, flight control, and airframe structure subsystems.
Author: BOEING CO RENTON WASH.
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Book Description
This specification defines the installed performance for the 475-pound-per-second size General Electric Company GE4/J5G engine in the Boeing Model 733-390 airplane and specifies the estimated inlet and nozzle drag values used for the determination of the airplane performance characteristics. System performance requirements established herein are design objectives to be applied in the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).
